A hypersonic vehicle model developed with piston theory

Collection of Technical Papers - 2006 Atmospheric Flight Mechanics Conference

Volumn 2, Issue , 2006, Pages 1241-1260

  Oppenheimer, Michael W ^a,b,c   Doman, David B ^a,b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b Control Theory and Optimization Branch ^*  (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLOW OF FLUIDS; MOTION ESTIMATION; PISTONS; PRANDTL NUMBER; PRESSURE MEASUREMENT; VELOCITY MEASUREMENT;

MACH NUMBER FLOWS; NEWTONIAN IMPACT THEORY; PISTON THEORY; PRANDTL-MEYER FLOW;

HYPERSONIC AERODYNAMICS;

EID: 33751395937     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-6637     Document Type: Conference Paper

References (5)

1. Lighthill, M., "Oscillating Airfoils at High Mach Number," Journal of the Aeronautical Sciences, Vol. 20, No. 6, 1953, pp. 402-406.
2. Ashley, H. and Zartarian, G., "Piston Theory - A New Aerodynamic Tool for the Aeroelastician," Journal of the Aeronautical Sciences, 1956, pp. 1109-1118.
3. Tarpley, C. and Lewis, M., "Stability Derivatives for a Hypersonic Caret-Wing Waverider," Journal of Aircraft, Vol. 32, No. 4, 1995, pp. 795-803.
4. Bolender, M. A. and Doman, D. B., "A Non-Linear Model for the Longitudinal Dynamics of a Hypersonic Airbreathing Vehicle," Proceedings of the 8005 Guidance, Navigation and Control Conference, AIAA Paper No. 2005-6255, August 2005.
5. Chavez, F. and Schmidt, D., "Analytical Aeropropulsive/Aeroelastic Hypersonic-Vehicle Model with Dynamic Analysis," Journal of Guidance, Control, and Dynamics, Vol. 17, No. 6, 1994, pp. 1308-1319.